What was found
WHILE REMOVING LT O/B FLAP HINGE ARM ASSEMBLIES AT WS 178.00 AND 264.00, FOUND HARDWARE TO BE CORRODED. (C-CHECK) RO 2/17/2021. RECEIVED SERVICEABLE PARTS. REFERENCE CAMP 21819156-1 FOR INSTALL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE REMOVING LT O/B FLAP HINGE ARM ASSEMBLIES AT WS 178.00 AND 264.00, FOUND HARDWARE TO BE CORRODED. (C-CHECK) RO 2/17/2021. RECEIVED SERVICEABLE PARTS. REFERENCE CAMP 21819156-1 FOR INSTALL.